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molod |
1.1 |
C $Header: $ |
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C $Name: $ |
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#include "FIZHI_OPTIONS.h" |
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subroutine gwdrag (myid,pz,pl,ple,dpres,pkz,uz,vz,tz,qz,phis_var, |
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. dudt,dvdt,dtdt,im,jm,lm,bi,bj,istrip,npcs,imglobal) |
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C*********************************************************************** |
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C |
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C PURPOSE: |
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C ======== |
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C Driver Routine for Gravity Wave Drag |
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C |
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C INPUT: |
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C ====== |
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C myid ....... Process ID |
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C pz ....... Surface Pressure [im,jm] |
| 16 |
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C pl ....... 3D pressure field [im,jm,lm] |
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C ple ....... 3d pressure at model level edges [im,jm,lm+1] |
| 18 |
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C dpres ....... pressure difference across level [im,jm,lm] |
| 19 |
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C pkz ....... pressure**kappa [im,jm,lm] |
| 20 |
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C uz ....... zonal velocity [im,jm,lm] |
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C vz ....... meridional velocity [im,jm,lm] |
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C tz ....... temperature [im,jm,lm] |
| 23 |
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C qz ....... specific humidity [im,jm,lm] |
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C phis_var .... topography variance |
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C im ....... number of grid points in x direction |
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C jm ....... number of grid points in y direction |
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C lm ....... number of grid points in vertical |
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C istrip ...... 'strip' length for cache size control |
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C npcs ....... number of strips |
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C imglobal .... (avg) number of longitude points around the globe |
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C |
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C INPUT/OUTPUT: |
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C ============ |
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C dudt ....... Updated U-Wind Tendency including Gravity Wave Drag |
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C dvdt ....... Updated V-Wind Tendency including Gravity Wave Drag |
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C dtdt ....... Updated Pi*Theta Tendency including Gravity Wave Drag |
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C |
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C*********************************************************************** |
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implicit none |
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#ifdef ALLOW_DIAGNOSTICS |
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#include "SIZE.h" |
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#include "DIAGNOSTICS_SIZE.h" |
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#include "DIAGNOSTICS.h" |
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#endif |
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c Input Variables |
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c --------------- |
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integer myid,im,jm,lm,bi,bj,istrip,npcs,imglobal |
| 50 |
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real pz(im,jm) |
| 51 |
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real pl(im,jm,lm) |
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real ple(im,jm,lm+1) |
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real dpres(im,jm,lm) |
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real pkz(im,jm,lm) |
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real uz(im,jm,lm) |
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real vz(im,jm,lm) |
| 57 |
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real tz(im,jm,lm) |
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real qz(im,jm,lm) |
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real phis_var(im,jm) |
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| 61 |
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real dudt(im,jm,lm) |
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real dvdt(im,jm,lm) |
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real dtdt(im,jm,lm) |
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c Local Variables |
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c --------------- |
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real tv(im,jm,lm) |
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real dragu(im,jm,lm), dragv(im,jm,lm) |
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real dragt(im,jm,lm) |
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real dragx(im,jm), dragy(im,jm) |
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real sumu(im,jm) |
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integer nthin(im,jm),nbase(im,jm) |
| 73 |
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integer nthini, nbasei |
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| 75 |
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real phis_std(im,jm) |
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| 77 |
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real std(istrip), ps(istrip) |
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real us(istrip,lm), vs(istrip,lm), ts(istrip,lm) |
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real dragus(istrip,lm), dragvs(istrip,lm) |
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real dragxs(istrip), dragys(istrip) |
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real plstr(istrip,lm),plestr(istrip,lm),dpresstr(istrip,lm) |
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integer nthinstr(istrip),nbasestr(istrip) |
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integer n,i,j,L |
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real getcon, pi |
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real grav, rgas, cp, cpinv, lstar |
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c Initialization |
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c -------------- |
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pi = 4.0*atan(1.0) |
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grav = getcon('GRAVITY') |
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rgas = getcon('RGAS') |
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cp = getcon('CP') |
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cpinv = 1.0/cp |
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lstar = 2*getcon('EARTH RADIUS')*cos(pi/3.0)/imglobal |
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c Compute NTHIN and NBASE |
| 98 |
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c ----------------------- |
| 99 |
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do j=1,jm |
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do i=1,im |
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do nthini = 1,lm+1 |
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if( 1000.0-ple(i,j,lm+2-nthini).gt.25. ) then |
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nthin(i,j) = nthini |
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goto 10 |
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endif |
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enddo |
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10 continue |
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do nbasei = 1,lm+1 |
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if( ple(i,j,lm+2-nbasei).lt.666.7 ) then |
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nbase(i,j) = nbasei |
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goto 20 |
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endif |
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enddo |
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20 continue |
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if( 666.7-ple(i,j,lm+2-nbase(i,j)) .gt. |
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. ple(i,j,lm+3-nbase(i,j))-666.7 ) then |
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nbase(i,j) = nbase(i,j)-1 |
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endif |
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| 121 |
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enddo |
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enddo |
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c Compute Topography Sub-Grid Standard Deviation |
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c ---------------------------------------------- |
| 125 |
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do j=1,jm |
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do i=1,im |
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phis_std(i,j) = min( 400.0, sqrt( max(0.0,phis_var(i,j)) )/grav ) |
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enddo |
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enddo |
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c Compute Virtual Temperatures |
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c ---------------------------- |
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do L = 1,lm |
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do j = 1,jm |
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do i = 1,im |
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tv(i,j,L) = tz(i,j,L)*pkz(i,j,L)*(1.+.609*qz(i,j,L)) |
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enddo |
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enddo |
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enddo |
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| 141 |
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c Call Gravity Wave Drag Paramterization on A-Grid |
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c ------------------------------------------------ |
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do n=1,npcs |
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call strip ( phis_std,std,im*jm,istrip,1,n ) |
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| 148 |
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call strip ( pz,ps,im*jm,istrip,1 ,n ) |
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call strip ( uz,us,im*jm,istrip,lm,n ) |
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call strip ( vz,vs,im*jm,istrip,lm,n ) |
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call strip ( tv,ts,im*jm,istrip,lm,n ) |
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call strip ( pl,plstr,im*jm,istrip,lm,n ) |
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call strip ( ple,plestr,im*jm,istrip,lm,n ) |
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call strip ( dpres,dpresstr,im*jm,istrip,lm,n ) |
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call stripint ( nthin,nthinstr,im*jm,istrip,lm,n ) |
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call stripint ( nbase,nbasestr,im*jm,istrip,lm,n ) |
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| 158 |
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call GWDD ( ps,us,vs,ts, |
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. dragus,dragvs,dragxs,dragys,std, |
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. plstr,plestr,dpresstr,grav,rgas,cp, |
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. istrip,lm,nthinstr,nbasestr,lstar ) |
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call paste ( dragus,dragu,istrip,im*jm,lm,n ) |
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call paste ( dragvs,dragv,istrip,im*jm,lm,n ) |
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call paste ( dragxs,dragx,istrip,im*jm,1 ,n ) |
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call paste ( dragys,dragy,istrip,im*jm,1 ,n ) |
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enddo |
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c Add Gravity-Wave Drag to Wind and Theta Tendencies |
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c -------------------------------------------------- |
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do L = 1,lm |
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do j = 1,jm |
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do i = 1,im |
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dragu(i,j,L) = sign( min(0.006,abs(dragu(i,j,L))),dragu(i,j,L) ) |
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dragv(i,j,L) = sign( min(0.006,abs(dragv(i,j,L))),dragv(i,j,L) ) |
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dragt(i,j,L) = -( uz(i,j,L)*dragu(i,j,L)+vz(i,j,L)*dragv(i,j,L) ) |
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. *cpinv |
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dudt(i,j,L) = dudt(i,j,L) + dragu(i,j,L) |
| 180 |
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dvdt(i,j,L) = dvdt(i,j,L) + dragv(i,j,L) |
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dtdt(i,j,L) = dtdt(i,j,L) + dragt(i,j,L)*pz(i,j)/pkz(i,j,L) |
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enddo |
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enddo |
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enddo |
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| 186 |
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c Compute Diagnostics |
| 187 |
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c ------------------- |
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if( igwdu.ne.0 .or. igwdv.ne.0 .or. igwdt.ne.0 ) then |
| 189 |
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do L = 1,lm |
| 190 |
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if( igwdu.ne.0 ) then |
| 191 |
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do j = 1,jm |
| 192 |
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do i = 1,im |
| 193 |
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qdiag(i,j,igwdu+L-1,bi,bj) = qdiag(i,j,igwdu+L-1,bi,bj) + |
| 194 |
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. dragu(i,j,L)*86400 |
| 195 |
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enddo |
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enddo |
| 197 |
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endif |
| 198 |
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if( igwdv.ne.0 ) then |
| 199 |
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do j = 1,jm |
| 200 |
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do i = 1,im |
| 201 |
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qdiag(i,j,igwdv+L-1,bi,bj) = qdiag(i,j,igwdv+L-1,bi,bj) + |
| 202 |
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. dragv(i,j,L)*86400 |
| 203 |
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enddo |
| 204 |
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enddo |
| 205 |
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endif |
| 206 |
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if( igwdt.ne.0 ) then |
| 207 |
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do j = 1,jm |
| 208 |
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do i = 1,im |
| 209 |
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qdiag(i,j,igwdt+L-1,bi,bj) = qdiag(i,j,igwdt+L-1,bi,bj) + |
| 210 |
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. dragt(i,j,L)*86400 |
| 211 |
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enddo |
| 212 |
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enddo |
| 213 |
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endif |
| 214 |
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enddo |
| 215 |
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endif |
| 216 |
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| 217 |
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c Gravity Wave Drag at Surface (U-Wind) |
| 218 |
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c ------------------------------------- |
| 219 |
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if( igwdus.ne.0 ) then |
| 220 |
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do j = 1,jm |
| 221 |
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do i = 1,im |
| 222 |
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qdiag(i,j,igwdus,bi,bj) = qdiag(i,j,igwdus,bi,bj) + dragx(i,j) |
| 223 |
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enddo |
| 224 |
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enddo |
| 225 |
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endif |
| 226 |
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| 227 |
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c Gravity Wave Drag at Surface (V-Wind) |
| 228 |
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c ------------------------------------- |
| 229 |
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if( igwdvs.ne.0 ) then |
| 230 |
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do j = 1,jm |
| 231 |
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do i = 1,im |
| 232 |
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qdiag(i,j,igwdvs,bi,bj) = qdiag(i,j,igwdvs,bi,bj) + dragy(i,j) |
| 233 |
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enddo |
| 234 |
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enddo |
| 235 |
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endif |
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| 237 |
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c Gravity Wave Drag at Model Top (U-Wind) |
| 238 |
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c --------------------------------------- |
| 239 |
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if( igwdut.ne.0 ) then |
| 240 |
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do j = 1,jm |
| 241 |
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do i = 1,im |
| 242 |
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sumu(i,j) = 0.0 |
| 243 |
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enddo |
| 244 |
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enddo |
| 245 |
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do L = 1,lm |
| 246 |
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do j = 1,jm |
| 247 |
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do i = 1,im |
| 248 |
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sumu(i,j) = sumu(i,j) + dragu(i,j,L)*dpres(i,j,L)/pz(i,j) |
| 249 |
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enddo |
| 250 |
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enddo |
| 251 |
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enddo |
| 252 |
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do j = 1,jm |
| 253 |
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do i = 1,im |
| 254 |
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qdiag(i,j,igwdut,bi,bj) = qdiag(i,j,igwdut,bi,bj) + dragx(i,j) |
| 255 |
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. + sumu(i,j)*pz(i,j)/grav*100 |
| 256 |
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enddo |
| 257 |
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enddo |
| 258 |
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endif |
| 259 |
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| 260 |
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c Gravity Wave Drag at Model Top (V-Wind) |
| 261 |
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c --------------------------------------- |
| 262 |
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if( igwdvt.ne.0 ) then |
| 263 |
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do j = 1,jm |
| 264 |
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do i = 1,im |
| 265 |
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sumu(i,j) = 0.0 |
| 266 |
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enddo |
| 267 |
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enddo |
| 268 |
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do L = 1,lm |
| 269 |
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do j = 1,jm |
| 270 |
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do i = 1,im |
| 271 |
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sumu(i,j) = sumu(i,j) + dragv(i,j,L)*dpres(i,j,L)/pz(i,j) |
| 272 |
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enddo |
| 273 |
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enddo |
| 274 |
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enddo |
| 275 |
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do j = 1,jm |
| 276 |
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do i = 1,im |
| 277 |
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qdiag(i,j,igwdvt,bi,bj) = qdiag(i,j,igwdvt,bi,bj) + dragy(i,j) |
| 278 |
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. + sumu(i,j)*pz(i,j)/grav*100 |
| 279 |
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enddo |
| 280 |
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enddo |
| 281 |
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endif |
| 282 |
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| 283 |
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ngwdu = ngwdu + 1 |
| 284 |
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ngwdv = ngwdv + 1 |
| 285 |
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ngwdt = ngwdt + 1 |
| 286 |
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ngwdus = ngwdus + 1 |
| 287 |
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ngwdvs = ngwdvs + 1 |
| 288 |
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ngwdut = ngwdut + 1 |
| 289 |
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ngwdvt = ngwdvt + 1 |
| 290 |
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| 291 |
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return |
| 292 |
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end |
| 293 |
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SUBROUTINE GWDD ( ps,u,v,t,dudt,dvdt,xdrag,ydrag, |
| 294 |
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. std,pl,ple,dpres, |
| 295 |
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. grav,rgas,cp,irun,lm,nthin,nbase,lstar ) |
| 296 |
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C*********************************************************************** |
| 297 |
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C |
| 298 |
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C Description: |
| 299 |
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C ============ |
| 300 |
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C Parameterization to introduce a Gravity Wave Drag |
| 301 |
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C due to sub-grid scale orographic forcing |
| 302 |
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C |
| 303 |
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C Input: |
| 304 |
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C ====== |
| 305 |
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C ps ......... Surface Pressure |
| 306 |
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C u .......... Zonal Wind (m/sec) |
| 307 |
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C v .......... Meridional Wind (m/sec) |
| 308 |
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C t .......... Virtual Temperature (deg K) |
| 309 |
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C std ........ Standard Deviation of sub-grid Orography (m) |
| 310 |
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C ple ....... Model pressure Edge Values |
| 311 |
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C pl ........ Model pressure Values |
| 312 |
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C dpres....... Model Delta pressure Values |
| 313 |
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C grav ....... Gravitational constant (m/sec**2) |
| 314 |
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C rgas ....... Gas constant |
| 315 |
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C cp ......... Specific Heat at constant pressure |
| 316 |
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C irun ....... Number of grid-points in horizontal dimension |
| 317 |
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C lm ......... Number of grid-points in vertical dimension |
| 318 |
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C lstar ...... Monochromatic Wavelength/(2*pi) |
| 319 |
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C |
| 320 |
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C Output: |
| 321 |
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C ======= |
| 322 |
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C dudt ....... Zonal Acceleration due to GW Drag (m/sec**2) |
| 323 |
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C dvdt ....... Meridional Acceleration due to GW Drag (m/sec**2) |
| 324 |
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C xdrag ...... Zonal Surface and Base Layer Stress (Pa) |
| 325 |
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C ydrag ...... Meridional Surface and Base Layer Stress (Pa) |
| 326 |
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C |
| 327 |
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C*********************************************************************** |
| 328 |
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| 329 |
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implicit none |
| 330 |
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| 331 |
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c Input Variables |
| 332 |
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c --------------- |
| 333 |
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integer irun,lm |
| 334 |
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real ps(irun) |
| 335 |
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real u(irun,lm), v(irun,lm), t(irun,lm) |
| 336 |
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real dudt(irun,lm), dvdt(irun,lm) |
| 337 |
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real xdrag(irun), ydrag(irun) |
| 338 |
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real std(irun) |
| 339 |
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real ple(irun,lm+1), pl(irun,lm), dpres(irun,lm) |
| 340 |
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real grav, rgas, cp |
| 341 |
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integer nthin(irun),nbase(irun) |
| 342 |
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real lstar |
| 343 |
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| 344 |
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c Dynamic Allocation Variables |
| 345 |
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c ---------------------------- |
| 346 |
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real ubar(irun), vbar(irun), robar(irun) |
| 347 |
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real speed(irun), ang(irun) |
| 348 |
|
|
real bv(irun,lm) |
| 349 |
|
|
real nbar(irun) |
| 350 |
|
|
|
| 351 |
|
|
real tstd(irun) |
| 352 |
|
|
real XTENS(irun,lm+1), YTENS(irun,lm+1) |
| 353 |
|
|
real TENSIO(irun,lm+1) |
| 354 |
|
|
real DRAGSF(irun) |
| 355 |
|
|
real RO(irun,lm), DZ(irun,lm) |
| 356 |
|
|
|
| 357 |
|
|
integer icrilv(irun) |
| 358 |
|
|
|
| 359 |
|
|
c Local Variables |
| 360 |
|
|
c --------------- |
| 361 |
|
|
integer i,l |
| 362 |
|
|
real a,g,stdmax,agrav,akwnmb |
| 363 |
|
|
real gocp,roave,roiave,frsf,gstar,vai1,vai2 |
| 364 |
|
|
real vaisd,velco,deluu,delvv,delve2,delz,vsqua |
| 365 |
|
|
real richsn,crifro,crif2,fro2,coef |
| 366 |
|
|
|
| 367 |
|
|
c Initialization |
| 368 |
|
|
c -------------- |
| 369 |
|
|
a = 1.0 |
| 370 |
|
|
g = 1.0 |
| 371 |
|
|
agrav = 1.0/GRAV |
| 372 |
|
|
akwnmb = 1.0/lstar |
| 373 |
|
|
gocp = GRAV/CP |
| 374 |
|
|
|
| 375 |
|
|
c Constrain the Maximum Value of the Standard Deviation |
| 376 |
|
|
c ----------------------------------------------------- |
| 377 |
|
|
stdmax = 400. |
| 378 |
|
|
do i = 1,irun |
| 379 |
|
|
tstd(i) = std(i) |
| 380 |
|
|
if( std(i).gt.stdmax ) tstd(i) = stdmax |
| 381 |
|
|
enddo |
| 382 |
|
|
|
| 383 |
|
|
c Compute Atmospheric Density |
| 384 |
|
|
c --------------------------- |
| 385 |
|
|
do l = 1,lm |
| 386 |
|
|
do i = 1,irun |
| 387 |
|
|
ro(i,l) = pl(i,l)/(rgas*t(i,lm+1-l)) |
| 388 |
|
|
enddo |
| 389 |
|
|
enddo |
| 390 |
|
|
|
| 391 |
|
|
c Compute Layer Thicknesses |
| 392 |
|
|
c ------------------------- |
| 393 |
|
|
do l = 2,lm |
| 394 |
|
|
do i = 1,irun |
| 395 |
|
|
roiave = ( 1./ro(i,l-1) + 1./ro(i,l) )*0.5 |
| 396 |
|
|
dz(i,l) = agrav*roiave*( pl(i,l-1)-pl(i,l) ) |
| 397 |
|
|
enddo |
| 398 |
|
|
enddo |
| 399 |
|
|
|
| 400 |
|
|
|
| 401 |
|
|
c****************************************************** |
| 402 |
|
|
c Surface and Base Layer Stress * |
| 403 |
|
|
c****************************************************** |
| 404 |
|
|
|
| 405 |
|
|
c Definition of Surface Wind Vector |
| 406 |
|
|
c --------------------------------- |
| 407 |
|
|
do i = 1,irun |
| 408 |
|
|
robar(i) = 0.0 |
| 409 |
|
|
ubar(i) = 0.0 |
| 410 |
|
|
vbar(i) = 0.0 |
| 411 |
|
|
enddo |
| 412 |
|
|
|
| 413 |
|
|
do i = 1,irun |
| 414 |
|
|
do L = 1,nbase(i)-1 |
| 415 |
|
|
robar(i) = robar(i) + ro(i,L) *(ple(i,L)-ple(i,L+1)) |
| 416 |
|
|
ubar(i) = ubar(i) + u(i,lm+1-L)*(ple(i,L)-ple(i,L+1)) |
| 417 |
|
|
vbar(i) = vbar(i) + v(i,lm+1-L)*(ple(i,L)-ple(i,L+1)) |
| 418 |
|
|
enddo |
| 419 |
|
|
enddo |
| 420 |
|
|
|
| 421 |
|
|
do i = 1,irun |
| 422 |
|
|
robar(i) = robar(i)/(ple(i,1)-ple(i,nbase(i))) * 100.0 |
| 423 |
|
|
ubar(i) = ubar(i)/(ple(i,1)-ple(i,nbase(i))) |
| 424 |
|
|
vbar(i) = vbar(i)/(ple(i,1)-ple(i,nbase(i))) |
| 425 |
|
|
|
| 426 |
|
|
speed(i) = SQRT( ubar(i)*ubar(i) + vbar(i)*vbar(i) ) |
| 427 |
|
|
ang(i) = ATAN2(vbar(i),ubar(i)) |
| 428 |
|
|
|
| 429 |
|
|
enddo |
| 430 |
|
|
|
| 431 |
|
|
c Brunt Vaisala Frequency |
| 432 |
|
|
c ----------------------- |
| 433 |
|
|
do i = 1,irun |
| 434 |
|
|
do l = 2,nbase(i) |
| 435 |
|
|
VAI1 = (T(i,lm+1-l)-T(i,lm+2-l))/DZ(i,l)+GOCP |
| 436 |
|
|
if( VAI1.LT.0.0 ) then |
| 437 |
|
|
VAI1 = 0.0 |
| 438 |
|
|
endif |
| 439 |
|
|
VAI2 = 2.0*GRAV/( T(i,lm+1-l)+T(i,lm+2-l) ) |
| 440 |
|
|
VSQUA = VAI1*VAI2 |
| 441 |
|
|
BV(i,l) = SQRT(VSQUA) |
| 442 |
|
|
enddo |
| 443 |
|
|
enddo |
| 444 |
|
|
|
| 445 |
|
|
c Stress at the Surface Level |
| 446 |
|
|
c --------------------------- |
| 447 |
|
|
do i = 1,irun |
| 448 |
|
|
nbar(i) = 0.0 |
| 449 |
|
|
enddo |
| 450 |
|
|
do i = 1,irun |
| 451 |
|
|
do l = 2,nbase(i) |
| 452 |
|
|
NBAR(i) = NBAR(i) + BV(i,l)*(pl(i,l-1)-pl(i,l)) |
| 453 |
|
|
enddo |
| 454 |
|
|
enddo |
| 455 |
|
|
|
| 456 |
|
|
do i = 1,irun |
| 457 |
|
|
NBAR(i) = NBAR(i)/(pl(i,1)-pl(i,nbase(i))) |
| 458 |
|
|
FRSF = NBAR(i)*tstd(i)/speed(i) |
| 459 |
|
|
|
| 460 |
|
|
if( speed(i).eq.0.0 .or. nbar(i).eq.0.0 ) then |
| 461 |
|
|
TENSIO(i,1) = 0.0 |
| 462 |
|
|
else |
| 463 |
|
|
GSTAR = G*FRSF*FRSF/(FRSF*FRSF+A*A) |
| 464 |
|
|
TENSIO(i,1) = GSTAR*(ROBAR(i)*speed(i)*speed(i)*speed(i)) |
| 465 |
|
|
. / (NBAR(i)*LSTAR) |
| 466 |
|
|
endif |
| 467 |
|
|
|
| 468 |
|
|
XTENS(i,1) = TENSIO(i,1) * cos(ang(i)) |
| 469 |
|
|
YTENS(i,1) = TENSIO(i,1) * sin(ang(i)) |
| 470 |
|
|
DRAGSF(i) = TENSIO(i,1) |
| 471 |
|
|
XDRAG(i) = XTENS(i,1) |
| 472 |
|
|
YDRAG(i) = YTENS(i,1) |
| 473 |
|
|
enddo |
| 474 |
|
|
|
| 475 |
|
|
c Check for Very thin lowest layer |
| 476 |
|
|
c -------------------------------- |
| 477 |
|
|
do i = 1,irun |
| 478 |
|
|
if( NTHIN(i).gt.1 ) then |
| 479 |
|
|
do l = 1,nthin(i) |
| 480 |
|
|
TENSIO(i,l) = TENSIO(i,1) |
| 481 |
|
|
XTENS(i,l) = XTENS(i,1) |
| 482 |
|
|
YTENS(i,l) = YTENS(i,1) |
| 483 |
|
|
enddo |
| 484 |
|
|
endif |
| 485 |
|
|
enddo |
| 486 |
|
|
|
| 487 |
|
|
c****************************************************** |
| 488 |
|
|
c Compute Gravity Wave Stress from NTHIN+1 to NBASE * |
| 489 |
|
|
c****************************************************** |
| 490 |
|
|
|
| 491 |
|
|
do i = 1,irun |
| 492 |
|
|
do l = nthin(i)+1,nbase(i) |
| 493 |
|
|
|
| 494 |
|
|
velco = 0.5*( (u(i,lm+1-l)*ubar(i) + v(i,lm+1-l)*vbar(i)) |
| 495 |
|
|
. + (u(i,lm+2-l)*ubar(i) + v(i,lm+2-l)*vbar(i)) ) |
| 496 |
|
|
. / speed(i) |
| 497 |
|
|
|
| 498 |
|
|
C Convert to Newton/m**2 |
| 499 |
|
|
roave = 0.5*(ro(i,l-1)+ro(i,l)) * 100.0 |
| 500 |
|
|
|
| 501 |
|
|
if( VELCO.le.0.0 ) then |
| 502 |
|
|
TENSIO(i,l) = TENSIO(i,l-1) |
| 503 |
|
|
goto 1500 |
| 504 |
|
|
endif |
| 505 |
|
|
|
| 506 |
|
|
c Froude number squared |
| 507 |
|
|
c --------------------- |
| 508 |
|
|
FRO2 = bv(i,l)/(AKWNMB*ROAVE*VELCO*VELCO*VELCO)*TENSIO(i,l-1) |
| 509 |
|
|
DELUU = u(i,lm+1-l)-u(i,lm+2-l) |
| 510 |
|
|
DELVV = v(i,lm+1-l)-v(i,lm+2-l) |
| 511 |
|
|
DELVE2 = ( DELUU*DELUU + DELVV*DELVV ) |
| 512 |
|
|
|
| 513 |
|
|
c Compute Richarson Number |
| 514 |
|
|
c ------------------------ |
| 515 |
|
|
if( DELVE2.ne.0.0 ) then |
| 516 |
|
|
DELZ = DZ(i,l) |
| 517 |
|
|
VSQUA = BV(i,l)*BV(i,l) |
| 518 |
|
|
RICHSN = DELZ*DELZ*VSQUA/DELVE2 |
| 519 |
|
|
else |
| 520 |
|
|
RICHSN = 99999.0 |
| 521 |
|
|
endif |
| 522 |
|
|
|
| 523 |
|
|
if( RICHSN.le.0.25 ) then |
| 524 |
|
|
TENSIO(i,l) = TENSIO(i,l-1) |
| 525 |
|
|
goto 1500 |
| 526 |
|
|
endif |
| 527 |
|
|
|
| 528 |
|
|
c Stress in the Base Layer changes if the local Froude number |
| 529 |
|
|
c exceeds the Critical Froude number |
| 530 |
|
|
c ---------------------------------- |
| 531 |
|
|
CRIFRO = 1.0 - 0.25/RICHSN |
| 532 |
|
|
CRIF2 = CRIFRO*CRIFRO |
| 533 |
|
|
if( l.eq.2 ) CRIF2 = MIN(0.7,CRIF2) |
| 534 |
|
|
|
| 535 |
|
|
if( FRO2.gt.CRIF2 ) then |
| 536 |
|
|
TENSIO(i,l) = CRIF2/FRO2*TENSIO(i,l-1) |
| 537 |
|
|
else |
| 538 |
|
|
TENSIO(i,l) = TENSIO(i,l-1) |
| 539 |
|
|
endif |
| 540 |
|
|
|
| 541 |
|
|
1500 CONTINUE |
| 542 |
|
|
XTENS(i,l) = TENSIO(i,l)*COS(ang(i)) |
| 543 |
|
|
YTENS(i,l) = TENSIO(i,l)*SIN(ang(i)) |
| 544 |
|
|
|
| 545 |
|
|
enddo |
| 546 |
|
|
enddo |
| 547 |
|
|
|
| 548 |
|
|
c****************************************************** |
| 549 |
|
|
c Compute Gravity Wave Stress from Base+1 to Top * |
| 550 |
|
|
c****************************************************** |
| 551 |
|
|
|
| 552 |
|
|
do i = 1,irun |
| 553 |
|
|
icrilv(i) = 0 |
| 554 |
|
|
enddo |
| 555 |
|
|
|
| 556 |
|
|
do i = 1,irun |
| 557 |
|
|
do l = nbase(i)+1,lm+1 |
| 558 |
|
|
|
| 559 |
|
|
TENSIO(i,l) = 0.0 |
| 560 |
|
|
|
| 561 |
|
|
c Check for Critical Level Absorption |
| 562 |
|
|
c ----------------------------------- |
| 563 |
|
|
if( icrilv(i).eq.1 ) goto 130 |
| 564 |
|
|
|
| 565 |
|
|
c Let Remaining Stress escape out the top edge of model |
| 566 |
|
|
c ----------------------------------------------------- |
| 567 |
|
|
if( l.eq.lm+1 ) then |
| 568 |
|
|
TENSIO(i,l) = TENSIO(i,l-1) |
| 569 |
|
|
goto 130 |
| 570 |
|
|
endif |
| 571 |
|
|
|
| 572 |
|
|
ROAVE = 0.5*(ro(i,l-1)+ro(i,l)) * 100.0 |
| 573 |
|
|
VAI1 = (T(i,lm+1-l)-T(i,lm+2-l))/DZ(i,l)+GOCP |
| 574 |
|
|
|
| 575 |
|
|
if( VAI1.lt.0.0 ) then |
| 576 |
|
|
icrilv(i) = 1 |
| 577 |
|
|
TENSIO(i,l) = 0.0 |
| 578 |
|
|
goto 130 |
| 579 |
|
|
endif |
| 580 |
|
|
|
| 581 |
|
|
VAI2 = 2.0*GRAV/(T(i,lm+1-l)+T(i,lm+2-l)) |
| 582 |
|
|
VSQUA = VAI1*VAI2 |
| 583 |
|
|
VAISD = SQRT(VSQUA) |
| 584 |
|
|
|
| 585 |
|
|
velco = 0.5*( (u(i,lm+1-l)*ubar(i) + v(i,lm+1-l)*vbar(i)) |
| 586 |
|
|
. + (u(i,lm+2-l)*ubar(i) + v(i,lm+2-l)*vbar(i)) ) |
| 587 |
|
|
. / speed(i) |
| 588 |
|
|
|
| 589 |
|
|
if( velco.lt.0.0 ) then |
| 590 |
|
|
icrilv(i) = 1 |
| 591 |
|
|
TENSIO(i,l) = 0.0 |
| 592 |
|
|
goto 130 |
| 593 |
|
|
endif |
| 594 |
|
|
|
| 595 |
|
|
c Froude number squared |
| 596 |
|
|
c --------------------- |
| 597 |
|
|
FRO2 = vaisd/(AKWNMB*ROAVE*VELCO*VELCO*VELCO)*TENSIO(i,l-1) |
| 598 |
|
|
DELUU = u(i,lm+1-l)-u(i,lm+2-l) |
| 599 |
|
|
DELVV = v(i,lm+1-l)-v(i,lm+2-l) |
| 600 |
|
|
DELVE2 = ( DELUU*DELUU + DELVV*DELVV ) |
| 601 |
|
|
|
| 602 |
|
|
c Compute Richarson Number |
| 603 |
|
|
c ------------------------ |
| 604 |
|
|
if( DELVE2.ne.0.0 ) then |
| 605 |
|
|
DELZ = DZ(i,l) |
| 606 |
|
|
RICHSN = DELZ*DELZ*VSQUA/DELVE2 |
| 607 |
|
|
else |
| 608 |
|
|
RICHSN = 99999.0 |
| 609 |
|
|
endif |
| 610 |
|
|
|
| 611 |
|
|
if( RICHSN.le.0.25 ) then |
| 612 |
|
|
TENSIO(i,l) = 0.0 |
| 613 |
|
|
icrilv(i) = 1 |
| 614 |
|
|
goto 130 |
| 615 |
|
|
endif |
| 616 |
|
|
|
| 617 |
|
|
c Stress in Layer changes if the local Froude number |
| 618 |
|
|
c exceeds the Critical Froude number |
| 619 |
|
|
c ---------------------------------- |
| 620 |
|
|
CRIFRO = 1.0 - 0.25/RICHSN |
| 621 |
|
|
CRIF2 = CRIFRO*CRIFRO |
| 622 |
|
|
|
| 623 |
|
|
if( FRO2.ge.CRIF2 ) then |
| 624 |
|
|
TENSIO(i,l) = CRIF2/FRO2*TENSIO(i,l-1) |
| 625 |
|
|
else |
| 626 |
|
|
TENSIO(i,l) = TENSIO(i,l-1) |
| 627 |
|
|
endif |
| 628 |
|
|
|
| 629 |
|
|
130 continue |
| 630 |
|
|
XTENS(i,l) = TENSIO(i,l)*COS(ang(i)) |
| 631 |
|
|
YTENS(i,l) = TENSIO(i,l)*SIN(ang(i)) |
| 632 |
|
|
enddo |
| 633 |
|
|
enddo |
| 634 |
|
|
|
| 635 |
|
|
C ****************************************************** |
| 636 |
|
|
C MOMENTUM CHANGE FOR FREE ATMOSPHERE * |
| 637 |
|
|
C ****************************************************** |
| 638 |
|
|
|
| 639 |
|
|
do i = 1,irun |
| 640 |
|
|
do l = nthin(i)+1,lm |
| 641 |
|
|
coef = -grav*ple(i,lm+1)/dpres(i,lm+1-l) |
| 642 |
|
|
dudt(i,lm+1-l) = coef*(XTENS(i,l+1)-XTENS(i,l)) |
| 643 |
|
|
dvdt(i,lm+1-l) = coef*(YTENS(i,l+1)-YTENS(i,l)) |
| 644 |
|
|
enddo |
| 645 |
|
|
enddo |
| 646 |
|
|
|
| 647 |
|
|
c Momentum change near the surface |
| 648 |
|
|
c -------------------------------- |
| 649 |
|
|
do i = 1,irun |
| 650 |
|
|
coef = grav*ple(i,lm+1)/(ple(i,lm+1-nthin(i))-ple(i,lm+1)) |
| 651 |
|
|
dudt(i,lm) = coef*(XTENS(i,nthin(i)+1)-XTENS(i,1)) |
| 652 |
|
|
dvdt(i,lm) = coef*(YTENS(i,nthin(i)+1)-YTENS(i,1)) |
| 653 |
|
|
enddo |
| 654 |
|
|
|
| 655 |
|
|
c If Lowest layer is very thin, it is strapped to next layer |
| 656 |
|
|
c ---------------------------------------------------------- |
| 657 |
|
|
do i = 1,irun |
| 658 |
|
|
if( nthin(i).gt.1 ) then |
| 659 |
|
|
do l = 2,nthin(i) |
| 660 |
|
|
dudt(i,lm+1-l) = dudt(i,lm) |
| 661 |
|
|
dvdt(i,lm+1-l) = dvdt(i,lm) |
| 662 |
|
|
enddo |
| 663 |
|
|
endif |
| 664 |
|
|
enddo |
| 665 |
|
|
|
| 666 |
|
|
c Convert Units to (m/sec**2) |
| 667 |
|
|
c --------------------------- |
| 668 |
|
|
do l = 1,lm |
| 669 |
|
|
do i = 1,irun |
| 670 |
|
|
dudt(i,l) = - dudt(i,l)/ps(i)*0.01 |
| 671 |
|
|
dvdt(i,l) = - dvdt(i,l)/ps(i)*0.01 |
| 672 |
|
|
enddo |
| 673 |
|
|
enddo |
| 674 |
|
|
|
| 675 |
|
|
return |
| 676 |
|
|
end |
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